Samara University Repository
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This is an open electronic archive created to preserve and disseminate the scientific results of our university. The works of researchers, faculty members, and students are available to everyone for academic and research purposes.
The repository contains dissertations, research articles, educational and methodological materials, monographs, and regulatory documents. The collections cover a wide range of fields: from aerospace technologies, engine engineering, and computer science to history, linguistics, mathematics, and ecology. The archive brings together the scientific heritage of the university, including materials prepared during the period of Samara State Aerospace University and Samara State University.
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| Title: | Учет покрытий элементов проточной части при прогнозировании характеристик компрессоров и турбин ГТД |
| Authors: | Михеев М. Г. Шипунов В. В. |
| Keywords: | compressors flow path gas dynamic calculations gas turbine engines multilayer thermal protective coatings numerical modeling performance prediction surface roughness turbines turbomachine blades газодинамические расчеты газотурбинные двигатели компрессоры лопатки турбомашин многослойные термозащитные покрытия прогнозирование характеристик проточная часть турбины численное моделирование шероховатость поверхности |
| Issue Date: | 2025 |
| Citation: | Михеев, М. Г. Учет покрытий элементов проточной части при прогнозировании характеристик компрессоров и турбин ГТД = Taking into account the coatings of flowpath elements for definition the characteristics of compressors and turbines / М. Г. Михеев, В. В. Шипунов // Перспективы развития двигателестроения : материалы междунар. науч.-техн. конф. им. Н. Д. Кузнецова (18–20 июня 2025 г.) / Самар. нац. исслед. ун-т им. С. П. Королева (Самар. ун-т) ; редкол.: Е. В. Шахматов, А. И. Ермаков. - Самара : Изд-во Самар. ун-та, 2025. - С. 952-954. |
| Abstract: | Considering of 3D CFD models features for calculating compressor and turbine characteristics taking into account roughness. The impact of wall roughness for compressor and turbine parameters is defined. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/43574 |
| Appears in Collections: | Перспективы развития двигателестроения |
| File | Size | Format | |
|---|---|---|---|
| 978-5-7883-2191-2_2025-952-954.pdf | 293.39 kB | Adobe PDF | View/Open |
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